View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 23439U 94085A 23332.43303002 -.00000030 00000-0 35426-3 0 9992
2 23439 64.8203 10.0503 0157074 181.1526 178.9056 11.27575614190840
| Epoch (UTC): | 28 November 2023 10:23:33 |
| Eccentricity: | 0.0157074 |
| inclination: | 64.8203° |
| perigee height: | 1890 km |
| apogee height: | 2154 km |
| right ascension of ascending node: | 10.0503° |
| argument of perigee: | 181.1526° |
| revolutions per day: | 11.27575614 |
| mean anomaly at epoch: | 178.9056° |
| orbit number at epoch: | 19084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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